The Effects of Tail-Tilt on the Yaw Stability of Baseline-V Blended Wing Body Aircraft / Nur Syazwani C.M and Rizal E.M. Nasir

This paper presents a study on the effects of tilting the tail on yaw stability performance of Baseline-V blended wing body (BWB) aircraft. The study on BWB aircraft began in UiTM in 2005 and a few designs of BWB aircraft have been studied and published. Recent progress on BWB study in UiTM indicate...

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Bibliographic Details
Main Authors: C.M., Nur Syazwani, M. Nasir, Rizal E.
Format: Article
Language:English
Published: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2017
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Online Access:http://ir.uitm.edu.my/id/eprint/39122/1/39122.pdf
http://ir.uitm.edu.my/id/eprint/39122/
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